ADCS & Navigation — Space Hardware Marketplace

Gyroscope Sensor for Measuring Angular Velocity Vector Projections 2

Redundant free form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control system. Sealed monoblock device,…

Gyroscope Sensor for Measuring Angular Velocity Vector Projections 3

Monoblock device includes electronic and optoelectronic modules and a block of sensitive elements containing three mutually orthogonal sensitive…

Gyroscope Sensor for Measuring Angular Velocity Vector Projections-4

Redundant free form gyroscopic angular velocity vector meter for spacecraft orientation and stabilization control system. An unsealed two-block…

Inertial Measurement Unit

• Measurement range±60°/s
• Scale point of the least category Errror0.0001

Sealed monoblock device including electronic and opto-electronic modules with a block of sensitive elements, containing three mutually orthogonal…

Kinetic Moment Reset System 1207

Kinetic moment reset system. Structurally, the product consists of: - 2 primary converters of the geomagnetic field PGP-3M,…

Backup Inertial Measuring Device

Sealed monoblock device including 3 small fiber optic gyroscopes and a set of electronic devices.

Electromagnet EM-IF-20

The core electromagnet for the stabilization equipment of the spacecraft with a harness on which the connector is…

Electromagnetic Unit (EMU) – Magnetic Torquer for Nanosatellites

Electromagnetic unit (EMU) - Magnetic Torquer for nanosatellites. There is an option to develop and supply EMU with…

Electromagnetic Unit (EMU) – Magnetic Torquer

Electromagnetic unit (EMU) - Magnetic Torquer There is an option to develop and supply EMU with magnetic moment…

Altitude Control System

• Orientation accuracy1 deg
• Knowledge of Orientation Accuracy0,1 deg
• Accuracy of stabilization on each axis30 deg. s/s

Use for spacecraft positioning in Space.

Retroreflector system for AC (spacecraft) Sentinel-3 (ESA)

• PurposeReflection of quantum-optical station radiation for precision spacecraft orbit determination
• Year of release2011
• HeritageFlown on ESA Sentinel-3 spacecraft

Seven-reflector retroreflector array for precision laser ranging of the ESA Sentinel-3 spacecraft.

Retroreflector system for “Luna-Globe” spacecraft

• PurposeRe-reflection of laser radiation for ground-to-spacecraft ranging
• Year of release2013
• HeritageDeveloped for Luna-Globe lunar mission

Interference-coated angle-reflector panel for laser ranging on the Luna-Globe lander/orbiter.

Retroreflector system “Pyramid” for “Condor-FKA” spacecraft

• PurposeRe-reflection of laser radiation toward ground station photodetector to calibrate onboard equipment
• Year of release2016
• HeritageDeveloped for Condor-FKA spacecraft

Compact four-reflector "Pyramid" retroreflector for onboard calibration on the Condor-FKA satellite.

Ring retroreflector system for “Glonass-K2” spacecraft

• PurposeMetrological control of GLONASS space-complex characteristics and calibration of ground measuring instruments
• Year of release2017
• HeritageDeveloped for GLONASS-K2 spacecraft

36-reflector ring panel for metrological control and calibration of the GLONASS-K2 navigation constellation.

Lens SOVA-5

Wide-angle 13-lens objective for detection of low-orbit space objects at altitudes from 120 to 500 km.

SX-SBOX ADCS Actuators (Microsatellite)

• ADCS control unit SX-SBOX-ADCU-01ARM Cortex-M4 160 MHz, hot-redundant, RTOS, ≤5 W, 220 g
• Reaction wheel SX-SBOX-RWH-50-2.0-01Max torque 0.05 N·m, momentum 2 N·m·s, 43 W peak, 3.2 kg
• Magnetorquers SX-SBOX-MTQSX-MT-1…SX-MT-30: dipole 1–30 A·m², 200–1200 g

Attitude-control actuators of the SX-SBOX suite for microsatellite platforms: ADCS control unit, reaction wheel, magnetorquers and a magnetorquer…

SX-SBOX ADCS Sensors (Microsatellite)

• Satellite navigation SX-SBOX-GNSS-01Position 10 m (σ), velocity 0.01 m/s, 2 W
• GNSS antenna SX-SBOX-AGG-011559–1607 MHz, gain ≥5.5 dB, RHCP, 61 g
• MEMS rate sensor SX-SBOX-AVS-MEMS-01Bias drift 2°/h, noise 0.15°/√h, 0.6 W, 75 g

Attitude-determination and navigation sensors of the SX-SBOX suite for microsatellite platforms: satellite navigation, GNSS antenna, MEMS and fiber-optic…

SXL-AIRTABLE-02 Spacecraft Relative-Motion Air Table

• TypeAir-bearing relative-motion table
• Overall dimensions5000 × 4000 × 3000 mm
• Active area1860 × 2480 mm

Air table for testing relative motion of spacecraft: a precision aluminium horizontal surface with an even grid of…